EP1497897B1 - Gegen photochromismus beständige materialien für optische geräte in plasmaumgebungen - Google Patents
Gegen photochromismus beständige materialien für optische geräte in plasmaumgebungen Download PDFInfo
- Publication number
- EP1497897B1 EP1497897B1 EP03724168.4A EP03724168A EP1497897B1 EP 1497897 B1 EP1497897 B1 EP 1497897B1 EP 03724168 A EP03724168 A EP 03724168A EP 1497897 B1 EP1497897 B1 EP 1497897B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- matrix
- ring laser
- laser gyroscope
- weight percent
- metal oxide
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/20—Filters
- G02B5/28—Interference filters
- G02B5/285—Interference filters comprising deposited thin solid films
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/08—Mirrors
- G02B5/0816—Multilayer mirrors, i.e. having two or more reflecting layers
- G02B5/0825—Multilayer mirrors, i.e. having two or more reflecting layers the reflecting layers comprising dielectric materials only
- G02B5/0833—Multilayer mirrors, i.e. having two or more reflecting layers the reflecting layers comprising dielectric materials only comprising inorganic materials only
Definitions
- the present invention is a ring laser gyroscope comprising an interference mirror, formed from a matrix including ZrO 2 and another large heat of formation material such as Al 2 O 3 .
- Laser mirrors such as interference mirrors used in ring laser gyroscopes, are continually exposed to a high-energy plasma environment that degrades the mirror by reducing the oxide (removing oxygen) and by inducing photochromic losses.
- Optical devices of this type are formed from a "quarter wave" stack of alternating 1 ⁇ 4 ⁇ -thickness layers of a relatively high index of refraction material and a relatively low index of refraction material. These layers of material are often deposited on a dielectric substrate by vacuum deposition processes.
- ZrO 2 zirconium oxide
- a layer of ZrO 2 is also often typically used as the top layer of the stack in interference mirrors.
- ZrO 2 has a relatively large heat of formation (about -131,490 gram calories/mole of oxygen), and exhibits a relatively high resistance to degradation in plasma environments.
- ZrO 2 is also compatible with the relatively high temperatures (e.g., 450°-550°C) to which the mirrors are exposed during other ring laser gyro manufacturing steps.
- Another approach for minimizing the degradation effects involves coating the top layer of the mirror stack with Al 2 O 3 , another relatively large heat of formation material (about -134,693 gram calories/mole of oxygen).
- the ZrO 2 tends to form a micro-crystalline structure when deposited. This micro-crystalline structure creates scattering sites, increasing the loss of the mirror.
- One known approach for preventing the formation of the crystalline structure and producing an amorphous, low-scatter material is to dope the ZrO 2 with small amounts of a second material such as SiO 2 . Doping the ZrO 2 with a relatively low amount (e.g., 5-15 weight %) of SiO 2 in this manner inhibits the micro-crystalline structure, thereby enabling relatively low loss, low scatter and long life mirrors.
- the bonding energy of Si0 2 is so different with respect to that of Zr0 2 , however, that the Si0 2 is reduced in the presence of a significant energy source such as a plasma environment. This interaction can lead to photochromic loss increase which can degrade the performance of the mirror. The result is a decrease in the performance of the ring laser gyro or other system in which the optical device is used.
- EP-A-372438 and US5646780 disclose a ring laser gyroscope comprising an interference mirror including a layer formed from a matrix comprising ZrO 2 .
- the present invention is a ring laser gyroscope, comprising an interference mirror having a top layer with a homogeneous matrix of material including Zr0 2 and an amount of a second metal oxide selected from the group of Hf0 2 , Ti0 2 , Nb 2 0 5 and Al 2 0 3 .
- the second metal oxide is incorporated into the matrix at 2 to 15 weight percent, preferably 4 to 11 weight percent, and most preferably 6 to 9 weight percent.
- the matrix of material consists essentially of Zr0 2 and Al 2 0 3 .
- SiO 2 is not considered a metal oxide.
- the amount of metal oxide in the material is an amount which is effective to minimize microcrystalline structure formation without significantly reducing the effective index of refraction of the material.
- SiO 2 is not included in the material matrix.
- One embodiment of the invention includes about 2-15 weight percent of Al 2 O 3 in the matrix.
- Another preferred embodiment includes about 4-11 weight percent of Al 2 O 3 in the matrix.
- Yet another embodiment of the invention includes about 6-9 weight percent Al 2 O 3 in the matrix.
- RF ion beam or other vapor deposition processes can be used to form the matrix of material.
- One preferred embodiment is a sputtering process (e.g., ion beam sputtering) where the composition of the deposited film mimics the composition of the target. It is anticipated that other deposition techniques can be used with modified compositions to compensate for different evaporation rates. Co-deposition techniques can also be used.
- Preferred embodiments of the invention consist solely of the ZrO 2 and Al 2 O 3 compounds described above. However, it is anticipated that other elements or compounds can be incorporated into the matrix of material as well. Introduction of dopants into the matrix is known to alter physical, optical and electrical properties of the material.
- an interference mirror having a top layer formed by a matrix of ZrO 2 and Al 2 O 3 having the composition described above exhibits relatively low loss, low scatter and long life characteristics in a plasma environment. The photochromic loss of the laser is thereby significantly reduced, enhancing the power output of the device.
- the thickness of the layer is determined by the particular application for which the interference mirror is designed (i.e., the wavelength of light desired to be reflected).
- Al 2 O 3 is the large heat of formation metal oxide incorporated into the matrix in the preferred embodiment of the invention described above.
- metal oxides can be effectively used for this purpose as well.
- one such metal oxide is hafnium dioxide (HfO 2 ), which has a heat of formation of -134,190 gram calories per mole per oxygen.
- suitable metal oxides include, for example, titanium dioxide (TiO 2 ) and niobium oxide (Nb 2 O 5 ).
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Optical Elements Other Than Lenses (AREA)
- Physical Vapour Deposition (AREA)
Claims (11)
- Ringlasergyroskop, welches einen Interferenzspiegel umfasst, der eine obere Schicht mit einer homogenen Matrix eines ZrO2 aufweisenden Materials und einem Anteil eines zweiten Metalloxids aufweist, wobei das zweite Metalloxid aus der Gruppe ausgewählt ist, die aus HfO2, TiO2, Nb2O5 und Al2O3 besteht.
- Ringlasergyroskop nach Anspruch 1, wobei der Anteil des zweiten Metalloxids in der Matrix des Materials ein zum Verringern einer Bildung mikrokristalliner Strukturen während der Interferenzspiegelherstellung wirksamer Anteil ist.
- Ringlasergyroskop nach Anspruch 2, wobei der Anteil des zweiten Metalloxids in der Matrix des Materials ein Anteil ist, der bewirkt, dass der Interferenzspiegel Charakteristika eines verhältnismäßig geringen photochromen Verhaltens zeigt.
- Ringlasergyroskop nach Anspruch 1, wobei das zweite Metalloxid Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 4, wobei die Matrix des Materials etwa 2 - 15 Gewichtsprozent Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 4, wobei die Matrix des Materials etwa 4 - 11 Gewichtsprozent Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 4, wobei die Matrix des Materials etwa 6 - 9 Gewichtsprozent Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 1, wobei die Matrix des Materials im Wesentlichen aus ZrO2 und Al2O3 besteht.
- Ringlasergyroskop nach Anspruch 8, wobei die Matrix des Materials etwa 2 - 15 Gewichtsprozent Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 8, wobei die Matrix des Materials etwa 4 - 11 Gewichtsprozent Al2O3 aufweist.
- Ringlasergyroskop nach Anspruch 8, wobei die Matrix des Materials etwa 6 - 9 Gewichtsprozent Al2O3 aufweist.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/131,881 US7760432B2 (en) | 2002-04-25 | 2002-04-25 | Photochromic resistant materials for optical devices in plasma environments |
| US131881 | 2002-04-25 | ||
| PCT/US2003/012526 WO2003092129A1 (en) | 2002-04-25 | 2003-04-23 | Photochromic resistant materials for optical devices in plasma environments |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1497897A1 EP1497897A1 (de) | 2005-01-19 |
| EP1497897B1 true EP1497897B1 (de) | 2018-02-14 |
Family
ID=29248639
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03724168.4A Expired - Lifetime EP1497897B1 (de) | 2002-04-25 | 2003-04-23 | Gegen photochromismus beständige materialien für optische geräte in plasmaumgebungen |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US7760432B2 (de) |
| EP (1) | EP1497897B1 (de) |
| JP (1) | JP2005524111A (de) |
| AU (1) | AU2003231044A1 (de) |
| WO (1) | WO2003092129A1 (de) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10739137B2 (en) | 2018-08-17 | 2020-08-11 | Honeywell International Inc. | Solid state ring laser gyroscope using rare-earth gain dopants in glassy hosts |
| US11385057B2 (en) | 2019-09-20 | 2022-07-12 | Honeywell International Inc. | Extra thick ultraviolet durability coating |
| US11962118B2 (en) | 2020-10-27 | 2024-04-16 | Honeywell International Inc. | Ultraviolet filter for ring laser gyroscope mirrors |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2658418A1 (de) * | 1976-12-23 | 1978-06-29 | Leybold Heraeus Gmbh & Co Kg | Verfahren zur herstellung von antireflexschichten auf acrylglaesern, nach dem verfahren hergestellter optischer koerper und verwendung des optischen koerpers |
| US5764416A (en) * | 1988-04-19 | 1998-06-09 | Litton Systems, Inc. | Fault tolerant antireflective coatings |
| EP0372438A3 (de) | 1988-12-05 | 1990-08-01 | Honeywell Inc. | UV- und plasmastabiler vielschichtiger, hochreflektierender dielektrischer Spiegel |
| DK0395912T3 (da) * | 1989-05-02 | 1993-12-06 | Lonza Ag | Sintringsdygtigt zirconiumoxidpulver og fremgangsmåde til dets fremstilling |
| RU2064206C1 (ru) * | 1991-12-26 | 1996-07-20 | Физический институт им.П.Н.Лебедева РАН | Лазерный экран электронно-лучевой трубки и способ его изготовления |
| US5457570A (en) * | 1993-05-25 | 1995-10-10 | Litton Systems, Inc. | Ultraviolet resistive antireflective coating of Ta2 O5 doped with Al2 O3 and method of fabrication |
| FR2712990B1 (fr) * | 1993-11-22 | 1996-04-05 | Commissariat Energie Atomique | Miroir à large bande et à haute réflectivité et procédé de réalisation d'un tel miroir. |
| US5646780A (en) * | 1994-08-24 | 1997-07-08 | Honeywell Inc. | Overcoat method and apparatus for ZRO2 mirror stacks |
| US5786611A (en) * | 1995-01-23 | 1998-07-28 | Lockheed Idaho Technologies Company | Radiation shielding composition |
| US5978141A (en) * | 1997-11-17 | 1999-11-02 | The United States Of America As Represented By The Secretary Of The Navy | Optical mirror particularly suited for a quantum well mirror |
| US6107239A (en) * | 1998-01-19 | 2000-08-22 | Luchuang Environment Protection Science Co. Ltd. | Heat resistant metallic oxide catalyst for reducing pollution emission |
| US6495844B1 (en) * | 2000-01-25 | 2002-12-17 | Welch Allyn, Inc. | Metal halide lamp for curing adhesives |
| US6424419B1 (en) * | 2000-07-28 | 2002-07-23 | Northrop Grumman Corporation | System and method for providing cavity length control of a ring laser gyroscope |
-
2002
- 2002-04-25 US US10/131,881 patent/US7760432B2/en not_active Expired - Lifetime
-
2003
- 2003-04-23 JP JP2004500377A patent/JP2005524111A/ja not_active Withdrawn
- 2003-04-23 EP EP03724168.4A patent/EP1497897B1/de not_active Expired - Lifetime
- 2003-04-23 AU AU2003231044A patent/AU2003231044A1/en not_active Abandoned
- 2003-04-23 WO PCT/US2003/012526 patent/WO2003092129A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| US7760432B2 (en) | 2010-07-20 |
| EP1497897A1 (de) | 2005-01-19 |
| US20030202248A1 (en) | 2003-10-30 |
| AU2003231044A1 (en) | 2003-11-10 |
| WO2003092129A1 (en) | 2003-11-06 |
| JP2005524111A (ja) | 2005-08-11 |
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